N750DH

Service difficulty reports not matched to an aircraft · 121

They name N750DH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N750DH' AND registry_match IS NULL
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DHLA200800120Light · loosePILOT REPORT, EMERGENCY EXIT LIGHTS ILLUMINATE PERIODICALLY WITH SWITCH IN THE ARMED POSITION. RESOLUTION, CONFIRMED. RESEATED COCKPIT EMERGENCY EXIT LIGHT. OPS CHECKS GOOD IAW MM 33-50-01.Nov 1, 2008 · N750DH · Boeing 7272M7 · Emergency LightingSDR DHL2008F00031Light · inoperativeL1 DOOR EMER EXIT LIGHT INOP. R&R EMER EXIT LIGHT ASSY OPS CHECK GOOD IAW MM 33-50-71. ACFT WAS GROUNDED. FLIGHT NR 820.Aug 26, 2008 · N750DH · Boeing 7272M7 · Emergency LightingSDR DHL2008F00029Skin · crackedL1 DOOR FRAME 303 9 CRACK ON INBOARD FASTENER HOLE INSIDE UPPER HINGE CUTOUT. REPAIRED L-1 DOOR FRAME BS 303.95 UPPER HINGE CUTOUT IAW EVA B253-00089 REV IR DATED 2 JULY 08 AND BOEING TELEX 1-864663355-15 WITH REPAIR SKETCH 1-864663355-12, FABRICATED CLIP ANGJul 8, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, Plate/SkinSDR DHL2008F00023Skin · corrodedLT WHEEL WELL BS 931.5 ABOVE STRINGER 18A CORROSION SPOT SKIN BLOWN WBL 70.5. INSTALLED REPAIR PARTS AT LT WHEEL WELL BS 931 5 ABOVE STRINGER 18A AREA WBL 70 5 IAW EVA B253-00083 REV 01 DATED 1 JULY 08 AND AVENGER REPORT AAS-SSR-08-017 REV B DATED JUNE 30, 20Jul 6, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, Plate/SkinSDR DHL2008F00028Skin · gougedFUSELAGE INNER SKIN BELOW UPPER HINGE IS GOUGED BS 303 STRINGER 12L TO 306.65 LT HAND. FABRICATED REPAIR AND INSTALLED IAW EVA B253-00086 REV 03 DATED 2 JULY 08 AND BOEING REPAIR SKETCH 1-364663355-12 IN CONJUNCTION WITH BOEING TELEX 1-864663355-B DATED 6-23-Jul 3, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, Plate/SkinSDR DHL2008F00015Angle · corrodedL-2 DOOR TAP INTERIOR ANGLE SUPPORT AND WEB ARE CORRODED (EXFOLIATION) BS 1040/1065. REMOVED AND REPLACED L-2 DOOR UPPER ANGLE SUPPORT WEB BEAM IAW B727 SRM 51-30-2 AND BOEING DRAWING 65-56992 REV V DATED 3/26/01. (A)Jun 26, 2008 · N750DH · Boeing 7272M7 · Passenger/Crew DoorsSDR DHL2008F00018Web · crackedL-1 DOOR LOWER FORWARD CORNER OF WEB HAS CRACK. CUT OUT DAMAGE L-1 DOOR LOWER FORWARD CORNER WEB IAW B727 SRM 51-40-3 FIG 1. FABRICATED DOUBLER REPAIR AND INSTALLED IN L-1 DOOR IAW EVA B252-00082 REV IR DATED 6/19/08. (A)Jun 25, 2008 · N750DH · Boeing 7272M7 · Passenger/Crew DoorsSDR DHL2008F00010Web · crackedL-1 DOOR LOWER FORWARD BOTTOM OF DOOR HAS CRACKED WEB. INSTALLED NEW LOWER WEB FROM L-1 DOOR WITH MATERIAL 7075-T6 .075 SIZE 37 5 X 8 AND PO 9007406 IAW B727 SRM 51-30-2 52-10-1 FIG 1 AND 51-10-1. (A)Jun 23, 2008 · N750DH · Boeing 7272M7 · Passenger/Crew DoorsSDR DHL2008F00014Keelbeam · corrodedSURFACE CORROSION FRONT LOWER CHORD CENTER OF KEEL BEAM BS 740. REMOVED AND REPLACED BS 740 LOWER CHORD T ANGLE P/N 69-4711Y2, PO 8180132 IAW B727 SRM 51-30-2. T-ANGLE ORIGINAL EVALUATED OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. (A)Jun 22, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, KeelSDR DHL2008F00021Beam · misinstalledHORIZONTAL WALKWAY BEAM LOWER CHORD LT SIDE, HAS SEVERAL FASTENERS BUCK TAIL FLAT, ALSO IMPROPER SIZE FASTENERS BETWEEN BS 312 AND BS 328. REMOVED AND REPLACED HORIZONTAL WALKWAY LOWER LT CHORD BS 312 TO 328 IAW B727 SRM 51-30-2. P/N 65-19861-7 (A)Jun 19, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, StructureSDR DHL2008F00011Shear Tie · crackedSHEAR TIE CRACKED AT HORIZONTAL WALKWAY BEAM AREA BS 328 STRINGER 26L. REPAIRED SHEAR TIE AT HORIZONTAL WALKWAY BEAM BS 328 STRINGER 26L IAW B727 SRM 53-10-4 FIG 15. (A)Jun 19, 2008 · N750DH · Boeing 7272M7 · Fuselage Internal Mounting StructureSDR DHL2008F00009Skin · bulgedBULGE AT BS 660 AND STRINGER 27R EXTERIOR SKIN. REMOVED FASTENERS AND SHEAR TIE, TEE AT BS 660 AND STRINGER 27R IAW B727 SRM 51-30-2. FOUND SHEAR TIE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. INSTALLED NEW PART WITH P/N 6943683-5 AND PO 8180177 IAW B727 SRMJun 16, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, Plate/SkinSDR DHL2008F00026Channel · corrodedCORROSION, NOSE GEAR TRUNNION WELL LT FORWARD C-CHANNEL BS 303. REMOVED CORROSION ON LT FORWARD C-CHANNEL BS 303 IAW B727 SRM 51-10-6. EVALUATED OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. REMOVED AND REPLACED C-CHANNEL IAW B727 SRM 51-30-2. (A)Jun 13, 2008 · N750DH · Boeing 7272M7 · Fuselage Miscellaneous StructureSDR DHL2008F00027Stringer · corrodedEXFOLIATED CORROSION ON STRINGER 28L CHANNEL BETWEEN BS 620 AND BS 640. REPAIRED STRINGER BS 620-640 STRINGER 28L IAW B727 SRM 53-10-3 FIG 1 DETAIL 1. (A)Jun 12, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, Longeron/StringerSDR DHL2008F00022Stringer · crackedSTRINGER 15R IS CRACKED AT BS 720B + 5 INCHES. CUT OUT DAMAGE AREA DIMENSION .625 AT STRINGER 15R 720B IAW SRM 53-10-3 FIG 5. FABRICATED CHANNEL USING 7075-T6 040 PO 9007282 DIMENSION 5.125" X 1" X 1", RADIUS FILLER USING 7075-T6 .090 PO 9006162 DIMENSION 2.Jun 12, 2008 · N750DH · Boeing 7272M7 · Fuselage Main, Longeron/StringerSDR DHL2008F00012Seat Track · corrodedCABIN SEAT TRACK BS 1166 TO 848 LBL 24-25 LIGHT CORROSION IN SEVERAL AREA AND MISSING PRIMER. REMOVED CORROSION ON SEAT TRACK BETWEEN BS 1050 TO 848 LBL 24.25 IAW SRM 51-10-6. AREA OF SEAT TRACK WITH ORIGINAL THICKNESS OF .300, MATERIAL LOSS .002, MATERIAL RJun 11, 2008 · N750DH · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2008F00008Skin · crackedLT WING UPPER LEADING EDGE WS 507 AFT CORNER OF HOOK CUT OUT IS CRACKED. REMOVED HOOK SEAL IAW B727 SRM 51-30-2. STOP DRILLED CRACK DIMENSION .250 IAW B727 SRM 51-10-1. CUT OUT STRAP DIMENSION 7.875" X 1.875" IAW B727 SRM 57-30-4 FIG 9. FABRICATED PLATE REJun 10, 2008 · N750DH · Boeing 7272M7 · Wing, Plate/SkinSDR DHL2008F00020Seat Track · corrodedPITTING CORROSION ON SEAT TRACK UPPERMOST SURFACE AT BS 1029 AND RBL 24. BLEND OUT AREA AT SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 3. FABRICATED NEW SECTION OF SEAT TRACK IAW SRM 53-10-5 FIG 1 AND 51-20-1 INSTALLED NEW SEAT TRACK SRM 53-10-5 FIG 1Jun 7, 2008 · N750DH · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2008F00025Hinge · crackedMAIN CARGO DOOR AFT HINGE SECTION IS CRACKED AT FUSELAGE SIDE BS 650. REMOVED AFT HINGE SECTION AT MAIN CARGO DOOR SIDE BS 650 AND INSTALLED NEW SECTION WITH MS 20001+16-7200 AND PO 9002527 DIMENSION 17 IAW BOEING 727-200 FREIGHTER MAINTENANCE MANUAL FIGURE 5Jun 6, 2008 · N750DH · Boeing 7272M7 · Fuselage, Door HingeSDR DHL2008F00024Bracket · crackedLT WING NR 1 KRUEGER FLAP ACTUATOR INBOARD AND OUTBOARD ATTACH BRACKETS ARE CRACKED IN THE CORNERS. REMOVED BRACKETS (2 EACH) IAW B727 SRM 51-30-2. FABRICATED BRACKETS WITH 2024-T3 .036 3.5" X 7.5" PO 9006767 IAW BOEING ENGINEERING DOCUMENT 65-16275 AND B72 May 31, 2008 · N750DH · Boeing 7272M7 · Leading Edge DevicesSDR DHLA200700093Overheat Loop · misroutedNR 1 STRUT OVERHEAT LIGHT AFTER T/O PERFORMED NORMAL SHUTDOWN NR 1 ENGINE PER PROCEDURE. FOUND 4 DUCT CONNECTIONS LEAKING ON DUCT FROM PRECOOLER TO THE ENG. REMOVED AND REINSTALLED DUCTS PER 727 M/M 36-00-01 (DUCTS WERE MIS-ALIGNED) ALSO FOUND NR 1 PYLON OVEDec 27, 2007 · N750DH · Boeing 7272M7 · Overheat DetectionSDR DHLA200700085Latch · lack of lubeFWD ENTRY DOOR WILL NOT LOCK IN OPEN POSITION. CLEANED AND LUBED FWD ENTRY DOOR LATCH ASSY. OPS CHECK NORMAL IAW AMM 52-11-01.Dec 17, 2007 · N750DH · Boeing 7272M7 · Passenger/Crew DoorsSDR DHLA200700078Rudder Control · malfunctionedLOWER RUDDER MOVED ON ITS OWN FAR TO THE LEFT AS COMPARED WITH THE UPPER RUDDER AS SEEN ON THE RUDDER POSITION INDICATORS DURING TAKEOFF ROLL. ACFT PULLED TO THE LEFT, UPPER RUDDER IND FAR RT. TRANSFERRED RUDDER POS IND TO DMI 31029 PER MEL 27-8 CAT C DDD12-Dec 8, 2007 · N750DH · Boeing 7272M7 · Rudder Control SystemSDR DHL2007750505Skin · dentedWHILE AT FLIGHTSTAR FOR AN A CHECK DISCREPANCY FUSELAGE REPAIR HAS BLIND FASTENERS INSTALLED AT STA 1203 STR22R AND DOUBLER IS DENTED. REMOVED PREVIOUS REPAIR IAW B727SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER FROM 2024-T3 .063" PO NR 9005089 DIM 11 1/2" BY Aug 13, 2007 · N750DH · Boeing 7272M7 · Fuselage Main, Plate/SkinSDR DHL2007750504Door Frame · corrodedC2 DOOR LWR AFT FRAME CORRODED. REMOVED DOOR AFT CORNER AND DISPLACED WEB TO GAIN ACCESS IAW B727 SRM 51-30-2. CUT-OUT DAMAGED SECTION OF FRAME DIM 13 1/2" BY 6" IAW B727 51-10-1 AND 51-40-3 FIG 1. FABRICATED NEW FRAME SECTION FROM 7075-T6 .063" PO NR 90053Aug 13, 2007 · N750DH · Boeing 7272M7 · Fuselage Main, StructureSDR DHL2007750503Web · dentedDURING A CHECK DISCREPANCY, LT TORQUE BOX UPPER WEB HAS 2 DENTS AT APPROX STA 1243. CUTOUT DAMAGED AREA TWO 4" DIM IAW B727 SRM 51-40-2 FIG 1. FAB REPAIR DOUBLERS TWO 7075-T6 .040 PO NR 9005551 6.5"DIA AND 4 NUT PLATE CHANNEL DIA 1" BY 6" IAW B727 SRM 51-40Aug 13, 2007 · N750DH · Boeing 7272M7 · Fuselage Miscellaneous StructureSDR DHL2007750502Support Angle · crackedAFT AIRSTAIRS BS 1243 LT UPPER SUPPORT ANGLE CRACKED INSIDE OF TORQUE BOX. REMOVED CRACKED ANGLE IAW B727 SRM 51-30-2 FIG7. FABRICATED NEW ANGLE 7075-0 .063 PO NR 9005314 29 1/4" BY 4 3/4" IAW B727 SRM 53-10-2 FIG 6 AND 51-20-1. HEAT TREATED NEW PART TO 707Aug 13, 2007 · N750DH · Boeing 7272M7 · Fuselage Miscellaneous StructureSDR DHL2007750001Shear Tie · corrodedWHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR AN A CHECK.REFERENCE ASTAR N/RS 093661,093687 DISCREPANCY: PILLOWING AT FASTENERS ON FUSELAGE SKIN BS 700 BETWEEN STRINGER 25R-26R. REMOVED SHEAR TIE AT BS 700 BETWEEN S25R-26R. REMOVED CORROSION ON INNER SKIN MAT LOSAug 13, 2007 · N750DH · Boeing 7272M7 · Fuselage Internal Mounting StructureSDR DHL2007750002Duct · leakingNR 1 FIRE HANDLE INTERMITTENTLY GOES OFF AFTER TAKEOFF. FOUND SIX STAGE DUCT LEAKING AT FIREWALL ABOVE FIRELOOP REMOVED AND REPLACED DEFECTIVE DUCTING IAW B727 M/M 36-00-01. PERFORMED ENG RUN NO LEAKS NOTED IAW ASTAR JRHCHPT 7. REMOVED AND REPLACED FIRE LOOJan 12, 2007 · N750DH · Boeing 7272M7 · Engine Bleed Air SystemSDR DHL2006750001Apu · malfunctionedLOST APU BLEED AIR DURING ENGINE NR 2 START. PERFORMED EMERGENCY START MALFUNCTION CHECKLIST. APU CONTINUED TO RUN "HOT" (640 DEGREES) IN STATIC CONDITION (NO LOAD). SHUT DOWN APU. HOT/BURNING SMELL IN COCKPIT, DISSIPATED FOLLOWING APU SHUTDOWN. TRANSFERNov 29, 2006 · N750DH · Boeing 7272M7 · APU Core EngineSDR 2006750001Wing · crackedWING CRACKED, REMOVED AND REPLACED LEFT WING.Apr 11, 2006 · N750DH · Boeing 7272M7 · Wing StructureSDR DHL2006750522Skin · debondedL/WING I/B FOREFLAP, I/B CLOSE OUT BROKEN W/UPPER SKIN DISBONDED AT I/B END. REMOVED PREVIOUS REPAIR AND FABBED FILLER APPROX 3 3/4 BY 8 1/2 DOUBLER APPROX 5 1/4 BY 10 1/4 FROM 2024 T3 .016 PO 9003142. CLEANED, PREPPED, PRIMED, BONDED, CLEANED, TREATED, ANDMar 28, 2006 · N750DH · Boeing 7272M7 · Trailing Edge FlapsSDR DHL2006750521Skin · gougedFOUND L WING I/B AILERON UPPER SKIN IS GOUGED AT WS 410. CUT OUT DAMAGED AREA DIM 2X2 AND FABBED REPAIR DOUBLER FROM MAT USE 2024 T3 .04 PO 9003055 AND DIM 5 1/3 BY 4 IAW B727 SRM 57-50-2 FIG NR 7 AND 57-50-5 FIG 5. TREATED AND PRIMED IAW B727 SRM 51-10-2. Mar 20, 2006 · N750DH · Boeing 7272M7 · AileronsSDR DHL2006750518Frame · dentedFOUND FRAME DENTED AT BS 700 STR 24 R. CUT OUT DAMAGED AREA SIZE 1 BY 3/4 ON FRAME STA 700 AT STR 24R IAW B727 SRM 51-10-1. FABBED REPAIR ANGLE FROM 7075-0 .063 SIZE 8 3/4 BY 3 1/2 PO 9002827 IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3. HEAT TREATED TMar 17, 2006 · N750DH · Boeing 7272M7 · Fuselage Main, FrameSDR DHL2006750517Frame · dentedFRAME DENTED AT BS 680 AT STR 24R. CUT OUT DAMAGED AREA SIZE 1 X 3/4 ON FRAME STA 680 AT STR 24R IAW B727 SRM 51-10-1. FABBED REPAIR ANGLE FROM 7075 .063 SIZE 8 3/4 X 3 1/2 PO 9002827 IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3. HEATED TO 7075 T6 .063 Mar 17, 2006 · N750DH · Boeing 7272M7 · Fuselage Main, FrameSDR DHL2006570519Frame · dentedFOUND FRAME DENTED AT BS 720A STR 25R. CUT OUT DAMAGED AREA SIZE 1 BY 1 ON FRAME STA 720A AT STR 25R IAW B727 SRM 51-10-1. FABBED REPAIR ANGLE FROM 7075-0 .063 SIZE 8 3/4 BY 3 1/2 PO 9002827 IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3. HEAT TREATED TO Mar 17, 2006 · N750DH · Boeing 7272M7 · Fuselage Main, FrameSDR DHL2006570516Skin · corrodedCORROSION BULGE LT WING UPPER SURFACE PANEL 10" FWD OF NR 6 SPOILER WS 300. CUT OUT DAMAGED AREA 4 BY 2 1/2 IAW B727 SRM 51-10-1. FABBED DOUBLER FROM 2024 T3 .050 PO 53081 SIZE 9 BY 4 1/2 AND FILLER FROM 2024 T3 .080 PO 9002727 SIZE 1 BY 3 3/4 AND 2ND FILLERMar 16, 2006 · N750DH · Boeing 7272M7 · Elevator Control SystemSDR DHL2006750513Skin · dentedLT T/E SIDE OF UPPER RUDDER DENTED AT RUDDER TAB COURT (2ND FROM BOTTOM). FOUND DENT TO BE OUT OF LIMITS, ROUTED OUT DAMAGED AREA SIZE 3/8 BY 3/4 IAW B727 SRM 51-10-01. FABBED DOUBLER FROM 2024 T3 SIZE 4 BY 6 PO 9002416 IAW B727 SRM 51-40-2 FIG 3. TREATED Mar 15, 2006 · N750DH · Boeing 7272M7 · Rudder, Plate/SkinSDR DHL2006750512Web · bentVERT STAB FWD TENSION TIE SUPPORT WEB BENT/STRESSED RT SIDE. REMOVED SUPPORT WEB ON VERT STAB FWD TENSION TIE RT SIDE IAW B727 SRM 51-30-2. FABBED WEB FROM 7075 T6 .032 SIZE 24 1/4 BY 6 PO 9002507 IAW B727 SRM 51-20-1 AND SRM 55-30-2. TREATED AND PRIMED PARMar 14, 2006 · N750DH · Boeing 7272M7 · Vertical Stabilizer Miscellaneous StructureSDR DHL2006570514Skin · crackedL/WING INB FLAP, REAR SPAR LOWER CORE SHOWS CRACK AT INB AFT FLAP ACTUATING ROD CUT OUT. CUT OUT DAMAGED AREA AND FABBED REPAIR ANGLE FROM BAC 1503 100046 PO 617555 DIM 46 BY 2 AND SPLICE FROM BAC1503-100046 PO 617555 DIM 10 BY 2 IAW B727 SRM 51-40-4 FIG 1. Mar 14, 2006 · N750DH · Boeing 7272M7 · Trailing Edge FlapsSDR DHL2006750515Skin · gougedRT WING OTBD FORE FLAP LEADING EDGE IS GOUGED AT WBL 442. CUT OUT DAMAGED AREA DIM 1 5/8 BY 1, FABBED REPAIR DOUBLER FROM 2024T3 .063 PO 9003110 DIM 4 1/16 BY 4. TREATED PRIMED AND INSTALLED DOUBLER IAW B727 SRM 57-50-4 FIG 1 51-10-2 AND 51-30-2.Mar 14, 2006 · N750DH · Boeing 7272M7 · Trailing Edge FlapsSDR DHL2006750508Torque Box · crackedTORQUE BOX FIN REAR SPAR CHORD LWR LT SIDE APPEARS TO BE CRACKED PASSED STOP DRILL HOLE STA BS 1303 LBL 22. C/W HFEC ON BS 1303 FRAME WEB IAW B727 NDTM PT6 51-00-00 FIG 23. FOUND 1/4" CRACK EXTENDING FROM PREVIOUS STOP DRILL HOLE. TOTAL CRACK LENGTH 1". NOMar 13, 2006 · N750DH · Boeing 7272M7 · Fuselage Main, StructureSDR DHL2006750509Skin · gougedNR 6 SLAT TRAILING EDGE IS GOUGED AT OUTBD HOOK. ROUTED OUT GOUGE .200 RADIUS BY 6" AREA FOUND TO BE OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 2. FABBED REPAIR DOUBLER FROM 7075 T6 A125 PO5096301 DIM 8 1/2 BY 3 1/2 IAW B727 SRM 57-50-3 FIG10. TREATED AND PRIMEMar 13, 2006 · N750DH · Boeing 7272M7 · Leading Edge DevicesSDR DHL2006750511Beam · crackedSTA 1183 BULKHEAD VERTICAL BEAM IS CRACKED AT AFT FLANGE INBD AND OUTBD SIDE RBL 36. STOP DRILLED 2 CRACKS IAW S/B 727-53-0192 REV 1 DATED MAY 30 1991. REMOVED GILLINER SUPPORT STRUCTURE FOR ACCESS IAW S/B 727-53-0192 REV 1 DATED MAY 30 1991. LOCATED AND DRMar 13, 2006 · N750DH · Boeing 7272M7 · Wing, Rib/BulkheadSDR DHL2006750510Skin · dentedNR 6 SLAT UPPER SKIN IS DENTED AT WING STA 560. FOUND DENT TO BE OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 2. REMOVED 2 RIBS FOR ACCESS AND CUT OUT DAMAGE AREA SIZE 2 1/4 BY 3 1/2 IAW B727 SRM 51-30-2 AND 57-50-3 FIG 1. FABBED DOUBLER FROM 2024 T3 .080 SIZE 7 Mar 13, 2006 · N750DH · Boeing 7272M7 · Wing, Plate/SkinSDR DHL2006750507Structure · dentedFOUND C2 DOOR FWD LWR END DENTED. REMOVED C-2 DOOR LWR FWD CORNER DEPRESSOR IAW B727 SRM 51-30-2. LOCATED AND DRILLED HOLES IAW B727 SRM 51-30-2 FIG NR 2. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW PART IAW B727 SRM 51-30-1 FIG NR 8, PN 65-5994Mar 13, 2006 · N750DH · Boeing 7272M7 · Cargo/Baggage DoorsSDR DHL2006750506Support Bracket · crackedNR 1 LE FLAP ACTUATOR TRUNNION SUPPORT BRACKET IS CRACKED OUTBOARD END. CONFIRMED CRACK. REMOVED SUPPORT BRACKET AT NR 1 L/E FLAP ACTUATOR TRUNNION OUTBOARD END FABBED NEW SUPPORT BRACKET FROM 7075 T6 .040 PO 9002590 DIM 8 1/8 BY 3 3/4 AND TREATED PRIMED ANDMar 12, 2006 · N750DH · Boeing 7272M7 · Trailing Edge FlapsSDR DHL2006750505Stiffener · crackedFOUND LEFT WING REAR SPAR VERTICAL STIFFENER AT WS 546 INB OF NR 2 SPOILER FITTING SUPPORT IS CRACKED FROM BOTTOM END. REMOVED AND REPLACED L WING REAR SPAR VERT STIFFENER AT WS 546 I/B OF NR 2 SPOILER FITTING SUPPORT IAW B727 SRM 51-30-2, LEAK CHECK GOOD IAWMar 12, 2006 · N750DH · Boeing 7272M7 · Wing Miscellaneous StructureSDR DHL2006750504Frame · corrodedAFT CARGO COMPT FRAME ANS SHEAR TIE ARE CORRODED WITH EXFOLIATION AND BROKEN FASTENERS AT STA 1166 BETWEEN STR 28L AND 28R. REMOVED AUX STRUCTURE FROM STA 1166 BULKHEAD IAW B727 SRM 51-30-2, CLEANED AREA AND REMOVED CORROSION, FOUND OUT OF LIMITS, MATL.LOSS .Mar 12, 2006 · N750DH · Boeing 7272M7 · Fuselage Main, FrameSDR DHL2006750503Skin · corrodedAFT CARGO COMPARTMENT, VHF ANTENNA DOUBLER HAS HEAVY CORROSION BETWEEN STR 30-29R, BETWEEN STA 1030-1050. REMOVED VHF ANTENNA AND DOUBLER BETWEEN STR 30-29R, AT STA 1030-1050 IAW B727 SRM 51-30-2. FOUND FUSE CORRODED, CUT OUT DAMAGED AREA, SIZE 2 X 3.5 INCHEMar 12, 2006 · N750DH · Boeing 7272M7 · Fuselage Main, Plate/Skin
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